• 0
    • ارسال درخواست
    • حذف همه
    • Industrial Standards
    • Defence Standards
  • درباره ما
  • درخواست موردی
  • فهرست استانداردها
    • Industrial Standards
    • Defence Standards
  • راهنما
  • Login
  • لیست خرید شما 0
    • ارسال درخواست
    • حذف همه
View Item 
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  •   YSE
  • Defence Standards
  • NASA - National Aeronautics and Space Administration (NASA)
  • View Item
  • All Fields
  • Title(or Doc Num)
  • Organization
  • Year
  • Subject
Advanced Search
JavaScript is disabled for your browser. Some features of this site may not work without it.

Archive

NASA-LLIS-1222

Lessons Learned - Understanding specific operational characteristics of selected design options (threaded Inserts)

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1998

Abstract: Description of Driving Event:
Galling of threaded fasteners was experienced in the qualification test program of the Z1 Truss. Fasteners intended to be removable on-orbit galled during test. The fasteners were installed in locking threaded inserts ("KEEN" type).
Root cause: The inherent effect of the "Keen"-type, upset thread design is to bite hard into the fastener. After repeated installation and removal, the fastener will gall. These inserts work best engaged once, and are excellent in this application.
URI: https://yse.yabesh.ir/std/handle/yse/82765
Subject: Parts Materials & Processes
Collections :
  • NASA - National Aeronautics and Space Administration (NASA)
  • Download PDF : (13.07Kb)
  • Show Full MetaData Hide Full MetaData
  • Statistics

    NASA-LLIS-1222

Show full item record

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:19:18Z
date available2017-09-04T16:19:18Z
date copyright09/30/1998
date issued1998
identifier otherTHVEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/82765
description abstractDescription of Driving Event:
Galling of threaded fasteners was experienced in the qualification test program of the Z1 Truss. Fasteners intended to be removable on-orbit galled during test. The fasteners were installed in locking threaded inserts ("KEEN" type).
Root cause: The inherent effect of the "Keen"-type, upset thread design is to bite hard into the fastener. After repeated installation and removal, the fastener will gall. These inserts work best engaged once, and are excellent in this application.
languageEnglish
titleNASA-LLIS-1222num
titleLessons Learned - Understanding specific operational characteristics of selected design options (threaded Inserts)en
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1998
contenttypefulltext
subject keywordsParts Materials & Processes
subject keywordsProcurement Small Business & Industrial Relations
subject keywordsRisk Management/Assessment
subject keywordsTest & Verification
subject keywordsTest Article
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian
 
DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian